System and Method for Distributed Airflow Sensing

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20200025646A1





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Disclosed herein is a distributed pressure sensor system that quickly detects and counters changes in lift, onset of stall, and flutter. The distributed pressure sensor system may employ a plurality of integrated pressure ports distributed across the span of a wing's leading edge to gather differential pressure measurements. Based on the differential pressure measurements, the distributed pressure sensor system can estimate torque on the fuselage to provide a more efficient estimate for changes in lift, onset of stall, and/or flutter. These estimates may be applied as feedback to the aircraft's control system, thereby eliminating the latency in the existing platform dynamics.

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Inventor Name Address # of filed Patents Total Citations
Griffin, Riley Manassas, US 6 2
Lieu, Michael Manassas, US 3 33

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